Part Details | AIRCRAFT GAS TURBINE ENGINE REAR FRAME
2840-01-364-2281 A frame used for and part of the rear section of an aircraft gas turbine engine. May include struts.
Alternate Parts: 6051T95G04, 2840-01-364-2281, 01-364-2281, 2840013642281, 013642281
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 14, 1992 | 01-364-2281 | 52347 ( FRAME, REAR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-364-2281
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6051T95G04 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-364-2281
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| OVERALL LENGTH | 4.517 INCHES MINIMUM AND 4.531 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 16.995 INCHES MINIMUM AND 17.005 INCHES MAXIMUM |
| INSIDE DIAMETER | 15.495 INCHES MINIMUM AND 15.535 INCHES MAXIMUM |
| NUMBER OF VARIABLE GUIDE VANES | 6 |
| REFERENCE DATA AND LITERATURE | T.O. 2J-J85-54, FIG 13, IND 1 |
| SPECIAL FEATURES | MAINFRAME COMPRESSOR SECTION; MUST CONFORM TO AS367 SAFETY WIRE, KEY WASHERS AND COTTER PIN |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABKV$$AAARX$$ACZLB |
| END ITEM IDENTIFICATION | J85 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME ASSEMBLY,TURBINE |